Delta IV Heavy

Delta IV Heavy
Delta IV Heavy launches from Vandenberg Space Force Base
FunctionOrbital heavy-lift launch vehicle
ManufacturerUnited Launch Alliance
Country of originUnited States
Cost per launchUS$350 million
NRO: US$440 million
Size
Height70.7 m (232 ft)
Diameter5.1 m (17 ft)
Width15.3 m (50 ft)
Mass733,000 kg (1,616,000 lb)
Stages2+
Capacity
Payload to LEO
Mass28,790 kg (63,470 lb)
Payload to GEO
Mass6,750 kg (14,880 lb)
Associated rockets
FamilyDelta
Comparable
Launch history
StatusRetired
Launch sites
Total launches16
Success(es)15
Partial failure(s)1
First flight21 December 2004 (USA-181)
Last flight9 April 2024 (NROL-70)
Carries passengers or cargo
Boosters (CBC)
No. boosters2
Height40.8 m (134 ft)
Diameter5.1 m (17 ft)
Empty mass26,000 kg (57,000 lb)
Gross mass226,400 kg (499,100 lb)
Propellant mass200,400 kg (441,800 lb)
Powered by1 RS-68A
Maximum thrust3,140 kN (710,000 lbf)
Total thrust6,280 kN (1,410,000 lbf)
Specific impulseSea level: 360 s (3.5 km/s)
Vacuum: 412 s (4.04 km/s)
Burn time242 seconds
PropellantLH2 / LOX
First stage (CBC)
Height40.8 m (134 ft)
Diameter5.1 m (17 ft)
Gross mass226,400 kg (499,100 lb)
Propellant mass200,400 kg (441,800 lb)
Powered by1 RS-68A
Maximum thrust3,140 kN (710,000 lbf)
Specific impulseSea level: 360 s (3.5 km/s)
Vacuum: 412 s (4.04 km/s)
Burn time328 seconds
PropellantLH2 / LOX
Second stage (DCSS)
Height13.7 m (45 ft)
Diameter5.1 m (17 ft) (LH2 tank) 3.2 m (10 ft) (LOX tank)
Gross mass30,700 kg (67,700 lb)
Propellant mass27,220 kg (60,010 lb)
Powered by1 RL10-B-2
Maximum thrust110 kN (25,000 lbf)
Specific impulse465.5 s (4.565 km/s)
Burn time1125 seconds
PropellantLH2 / LOX

The Delta IV Heavy (Delta 9250H) was an expendable heavy-lift launch vehicle, the largest type of the Delta IV family. It had the highest capacity of any operational launch vehicle in the world after the retirement of the Space Shuttle in 2011 until the Falcon Heavy debuted in 2018, and it was the world's third highest-capacity launch vehicle in operation at the time of its retirement in 2024. It was manufactured by United Launch Alliance (ULA) and was first launched in 2004. Delta IV Heavy was the last operating member of the Delta IV family, and its final flight was on 9 April 2024. It is succeeded by the Vulcan Centaur rocket.

The Delta IV Heavy first stage consisted of a central Common Booster Core (CBC), with two additional CBCs as liquid rocket boosters instead of the GEM-60 solid rocket motors used by the Delta IV Medium+ versions. At lift-off, all three rocket engines would operate at full thrust, and 44 seconds later the central engine would throttle down to 55% to conserve fuel until the other two engines separate. The latter engines burn out at 242 seconds after launch and are separated as the central engine throttles back up to full thrust. The central engine burns out 86 seconds later, and the second stage completed the ascent to orbit.

The launch vehicle used three RS-68 engines, one in the central core and one in each booster. On the last seconds of countdown, the liquid hydrogen fuel would flow through the engines and upwards along the booster body, and after the ignition that hydrogen inflamed, creating the characteristic fireball and charred look of the booster.